Study of Oblique Shock Wave Control by Surface Arc Discharge Plasma
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Shaanxi, People’s Republic of China
2. Australian Maritime College, University of Tasmania, 7248 Tasmania, Australia
Funder
Science Challenge Project
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056107
Reference25 articles.
1. Effect of an electrostatic field on boundary- layer transition.
2. Influence of a DC corona discharge on the airflow along an inclined flat plate
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4. Development and characterization of plasma actuators for high-speed jet control
5. Plasma Effect on Shocks Configuration in Compression Ramp
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